Presentation + Paper
24 August 2021 Optical test method for checking optomechanical design in early instrument models: Application to the RAX Spectrometer aboard JAXA’s MMX Mission
Author Affiliations +
Abstract
Verification of thermal-mechanical-optical design for optical instruments in space exploration is highly significant due to large temperature variation and exposure to high shock and vibration levels. Such instruments must be completely robust to these harsh environments, as there are usually no options for realignment. The JAXA Martian Moons eXploration (MMX) Mission is set for launch in 2024 with main objectives to study the Martian moons, Deimos and Phobos. A rover will acquire for the first time Raman spectra of the Phobos surface using the Raman Spectrometer for MMX (RAX) developed at DLR. The Structural-Thermal-Model (STM) of RAX presented an early opportunity to evaluate the robustness of the instrument optical alignment to thermal and mechanical environments. An interferometric method implementing dummy objectives with cross hairs was developed to enable inline six-DOF measurements at critical places within the STM before development model (DM) optics were manufactured.
Conference Presentation
© (2021) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Conor Ryan, Martin Pertenais, Ute Böttger, Maximilian Buder, Yuichiro Cho, Heinz-Wilhelm Hübers, Till Hagelschuer, Steve Rockstein, Selene Rodd-Routley, Fernando Rull, Susanne Schröder, and Friedrich Schrandt "Optical test method for checking optomechanical design in early instrument models: Application to the RAX Spectrometer aboard JAXA’s MMX Mission", Proc. SPIE 11820, Astronomical Optics: Design, Manufacture, and Test of Space and Ground Systems III, 118200N (24 August 2021); https://doi.org/10.1117/12.2594191
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KEYWORDS
Beam splitters

Sensors

Mirrors

Interfaces

Objectives

Spectroscopy

Instrument modeling

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